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VACA RIOS, John Jairo e CERÓN MUÑOZ, Hernán Darío. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, v. 161, p. 1-14, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2025.110135. Acesso em: 27 nov. 2025.
APA
Vaca Rios, J. J., & Cerón Muñoz, H. D. (2025). A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, 161, 1-14. doi:10.1016/j.ast.2025.110135
NLM
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2025 nov. 27 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135
Vancouver
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2025 nov. 27 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135
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DAUD FILHO, Antonio Carlos et al. Transition flight of a concept of lifting-wing quadcopter. The Aeronautical Journal, p. 1-21, 2024Tradução . . Disponível em: https://dx.doi.org/10.1017/aer.2024.100. Acesso em: 27 nov. 2025.
APA
Daud Filho, A. C., Silva, E. C. N., Silva, J. R., Caurin, G. A. de P., & Belo, E. M. (2024). Transition flight of a concept of lifting-wing quadcopter. The Aeronautical Journal, 1-21. doi:10.1017/aer.2024.100
NLM
Daud Filho AC, Silva ECN, Silva JR, Caurin GA de P, Belo EM. Transition flight of a concept of lifting-wing quadcopter [Internet]. The Aeronautical Journal. 2024 ; 1-21.[citado 2025 nov. 27 ] Available from: https://dx.doi.org/10.1017/aer.2024.100
Vancouver
Daud Filho AC, Silva ECN, Silva JR, Caurin GA de P, Belo EM. Transition flight of a concept of lifting-wing quadcopter [Internet]. The Aeronautical Journal. 2024 ; 1-21.[citado 2025 nov. 27 ] Available from: https://dx.doi.org/10.1017/aer.2024.100
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HIMENO, Fernando Henrique Tadashi e CARVALHO, A. E. B. Analyses of reynolds and mach number effects on Tollmien–Schlichting wave–bump interaction in subsonic flows. Journal of Fluid Mechanics, v. 998, p. 1-36, 2024Tradução . . Disponível em: http://dx.doi.org/10.1017/jfm.2024.675. Acesso em: 27 nov. 2025.
APA
Himeno, F. H. T., & Carvalho, A. E. B. (2024). Analyses of reynolds and mach number effects on Tollmien–Schlichting wave–bump interaction in subsonic flows. Journal of Fluid Mechanics, 998, 1-36. doi:10.1017/jfm.2024.675
NLM
Himeno FHT, Carvalho AEB. Analyses of reynolds and mach number effects on Tollmien–Schlichting wave–bump interaction in subsonic flows [Internet]. Journal of Fluid Mechanics. 2024 ; 998 1-36.[citado 2025 nov. 27 ] Available from: http://dx.doi.org/10.1017/jfm.2024.675
Vancouver
Himeno FHT, Carvalho AEB. Analyses of reynolds and mach number effects on Tollmien–Schlichting wave–bump interaction in subsonic flows [Internet]. Journal of Fluid Mechanics. 2024 ; 998 1-36.[citado 2025 nov. 27 ] Available from: http://dx.doi.org/10.1017/jfm.2024.675
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, v. 10, n. 7, p. 1-26, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070651. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2023). Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, 10( 7), 1-26. doi:10.3390/aerospace10070651
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2025 nov. 27 ] Available from: https://doi.org/10.3390/aerospace10070651
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2025 nov. 27 ] Available from: https://doi.org/10.3390/aerospace10070651
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PARRA, Hector G. et al. Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, v. 16, n. 11, p. 1-14, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16114343. Acesso em: 27 nov. 2025.
APA
Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, 16( 11), 1-14. doi:10.3390/en16114343
NLM
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2025 nov. 27 ] Available from: https://doi.org/10.3390/en16114343
Vancouver
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2025 nov. 27 ] Available from: https://doi.org/10.3390/en16114343
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REZENDE, Thiago Freisleben Ribeiro e AGUIRRE, Felipe Oliveira e MEDEIROS, Marcello Augusto Faraco de. Numerical analysis of a compressible fluid flow over an asymmetric GAP: a 2D case study. 2023, Anais.. São Carlos, SP: EESC-USP, 2023. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3779/2675. Acesso em: 27 nov. 2025.
APA
Rezende, T. F. R., Aguirre, F. O., & Medeiros, M. A. F. de. (2023). Numerical analysis of a compressible fluid flow over an asymmetric GAP: a 2D case study. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3779/2675
NLM
Rezende TFR, Aguirre FO, Medeiros MAF de. Numerical analysis of a compressible fluid flow over an asymmetric GAP: a 2D case study [Internet]. Anais. 2023 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3779/2675
Vancouver
Rezende TFR, Aguirre FO, Medeiros MAF de. Numerical analysis of a compressible fluid flow over an asymmetric GAP: a 2D case study [Internet]. Anais. 2023 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3779/2675
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 44, p. 1-22, 2022Tradução . . Disponível em: https://doi.org/10.1007/s40430-022-03924-x. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2022). Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 44, 1-22. doi:10.1007/s40430-022-03924-x
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
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EGUEA, João Paulo e SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, v. 96, p. 1-9, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105542. Acesso em: 27 nov. 2025.
APA
Eguea, J. P., Silva, G. P. G. da, & Catalano, F. M. (2020). Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, 96, 1-9. doi:10.1016/j.ast.2019.105542
NLM
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
Vancouver
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
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SILVA, Gabriel Pereira Gouveia da et al. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, v. 97, p. 1-11, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105642. Acesso em: 27 nov. 2025.
APA
Silva, G. P. G. da, Eguea, J. P., Croce, J. A. G., & Catalano, F. M. (2020). Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, 97, 1-11. doi:10.1016/j.ast.2019.105642
NLM
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
Vancouver
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
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BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 27 nov. 2025.
APA
Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
NLM
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-4200
Vancouver
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-4200
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BRAVO MOSQUERA, Pedro David et al. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, v. 86, p. 497-519, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.01.059. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, 86, 497-519. doi:10.1016/j.ast.2019.01.059
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-3850
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-3850
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MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Global instability analysis of a boundary layer flow over a small cavity. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3535. Acesso em: 27 nov. 2025.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2019). Global instability analysis of a boundary layer flow over a small cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3535
NLM
Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-3535
Vancouver
Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2019-3535
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RIBEIRO, Daniel Garcia e BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf. Acesso em: 27 nov. 2025.
APA
Ribeiro, D. G., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2019). Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
NLM
Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
Vancouver
Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
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REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 27 nov. 2025.
APA
Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
NLM
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2018-0759
Vancouver
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2018-0759
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ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 27 nov. 2025.
APA
Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
NLM
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2018-3799
Vancouver
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://doi.org/10.2514/6.2018-3799
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BRAVO MOSQUERA, Pedro David et al. Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, v. 80, p. 156-176, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2018.07.014. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., Díaz Vázquez, G., & Catalano, F. M. (2018). Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, 80, 156-176. doi:10.1016/j.ast.2018.07.014
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
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RIBEIRO, Daniel Garcia e CERÓN MUÑOZ, Hernán Darío e BRAVO MOSQUERA, Pedro David. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. 2018, Anais.. Rio de Janeiro, RJ: ABCM, 2018. Disponível em: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf. Acesso em: 27 nov. 2025.
APA
Ribeiro, D. G., Cerón Muñoz, H. D., & Bravo Mosquera, P. D. (2018). Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. In Proceedings of ENCIT. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
NLM
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
Vancouver
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 27 nov. 2025.
APA
Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
NLM
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Vancouver
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PELEGRINELI, Luis Antonio Vieira et al. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf. Acesso em: 27 nov. 2025.
APA
Pelegrineli, L. A. V., Liorbano, F. F., Natori, H. O. H., & Angélico, R. A. (2018). Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
NLM
Pelegrineli LAV, Liorbano FF, Natori HOH, Angélico RA. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
Vancouver
Pelegrineli LAV, Liorbano FF, Natori HOH, Angélico RA. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
; Cerón Muñoz, Hernán Darío 
